CN1742277B - Aircraft taxi planning system and method - Google Patents
Aircraft taxi planning system and method Download PDFInfo
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- CN1742277B CN1742277B CN02824336.6A CN02824336A CN1742277B CN 1742277 B CN1742277 B CN 1742277B CN 02824336 A CN02824336 A CN 02824336A CN 1742277 B CN1742277 B CN 1742277B
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Abstract
A taxi planning system for aircraft provides an intuitive user interface for entering and selecting taxi plans quickly and easily. The system includes predefined reduced selection menus that prompt the pilot with feasible taxi choices. Predefined standard routes allow the pilot to select a taxi route with a minimum of keystrokes and in a minimum of time. A display screen communicates the selection menus and standard routes to the pilot who makes a selection with as little as one keystroke. A database comprising a linked list structure facilitates a flexible system that is able to represent a wide variety of airport runways, taxiways, gates, ramps, and other airport structures. The selected taxi route is communicated to other aircraft systems such as head-down displays, head-up displays, flight management computers, communication systems, and the like.
Description
Technical field
The present invention relates to aircraft floor guidance system (SGS), and relate in particular to by menu structure being used for of constituting be the user interface that aircraft is selected the expectation taxi circuit apace on the airport.
Background technology
On the guiding field, ground of improving aircraft, there is obvious interest.After aircraft landing is to the runway on airport, next procedure be make aircraft taxi to the expectation destination passenger's gate of boarding/go out for example.The driver is mistaken easily or lost in a large amount of runways, taxiway, hardstand and the buildings of forming the airport.This problem is apparent in view and obvious especially at night on big airport, and this moment, a large amount of light made aircraft taxi arrive expectation destination difficulty more.
Effectively taxi operation saves time and money.When the airport became more crowded, aircraft spent the plenty of time usually and slides between runway and landing gate.If driver's mistake is turned, lost or enter wrong runway or taxiway unintentionally, coasting time even can be longer.In addition, mistake turning or navigation wrong move can cause other delayed flight on the airport.
A main performance of airport ground guidance capability is to present the easy-to-use airport map of driver.A kind of conventional method is to go up at following leading (head-down) display (HDD) that the place ahead, visual field of driver shows to show this map.The sliding path that the driver typically enters or selects to have ratified through the ground controller.Then this display is indicated the current position of aircraft and sliding path is shown to stack on airport map.This demonstration makes the driver understand aircraft to be positioned at situation where with respect to selected sliding path.The critical aspects that the actual aviation electronics of ground guiding realizes is to comprise a user interface usually, is input in the airborne SGS system so that intuitively and promptly air traffic control (ATC) radio is slided to instruct by driver or crew.
For ground is guided in the operation is acceptable, must to the aircraft crew member provide directly perceived and fast means so that be integrated together sliding that instruction is inserted in the guidance system of ground and the conventional airplane that operation and driver/unit are familiar with being operated.The driver strives for and makes the ground guiding of sliding planning step and the separation of flight course planning process.For regular line or armada operator, this typically causes tangible training burden.
Any aircraft taxi planning system not only can be finished to receive and slide the task of instruction, thereby but also will make user interface intuitively make the training time the shortest.Wish that also being convenient to quick taxi circuit selects and make the input error minimum.
Thereby its continuity target is to seek to reduce cost, to reduce and slide mistake, make the approach that training is the shortest, shorten coasting time and improve airport efficient.
Summary of the invention
In order to solve target above-mentioned and other target, taxi planning system of the present invention comprises that a kind of unique users interface and one comprise the runway of describing the airport and the database of information of taxiway.Planning is handled and the flight course planning processing integrates and adopt similar process sliding in the present invention.This sets up a kind of user interface intuitively and further foundation operated the upward acceptable planning realization of sliding, and this realization obviously reduces unit training time and cost.Adopt that to make input slide time of programming commands according to data input technology of the present invention the shortest and make that to slide planning wrong minimum.
According to an aspect of the present invention, provide a kind of aircraft taxi planning system, comprising: a user interface comprises: a display screen, and a selection input; The data storage part of data is slided on a storage airport; And the processor of and described display screen and described selection input communication, wherein said processor slides data according to described airport and the previous branch of sliding selects generation may slide branch's menu, and described processor is sent to described display screen with described menu, describedly slides branch and the aircraft position matches.
According to one aspect of the present invention, as the next integrated taxi planning system of the expansion of the flight management system (FMS) that aircraft is provided the flight course planning function.Page formatting of the present invention is the expansion of FMS page formatting that flight course planning is adopted preferably, thereby is intuitively and easy study for driver and crew.
In another aspect of the present invention, use choice menus to simplify the taxi circuit input and to reduce mistake.The invention provides the current location (for example runway or landing gate) of aircraft.This information be by driver's input in advance or receive from another aircraft system.This system preferably also provides destination (for example runway 27R or landing gate A25).Utilize these provisioning informations, the present invention searches related with this current location effectively sliding and selects and show to the driver as menu.Along with the driver selects the branch of sliding path, screen to spread out and present effectively to slide the menu that branch is selected.This processing is carried out sliding planning until finishing fast.In another embodiment, storage predefined canonical path and make available in storer.In another embodiment, receive predefined standard taxi circuit from ATC by the data link.
Another aspect of the present invention is to realize database structure of the present invention.This database structure preferably adopts the chained list that can realize the configuration of various airports flexibly.Can upgrade this database under the program software continually needn't changing.More preferably, the present invention uses the chained list of setting up from two tables of data.
According to another aspect of the present invention, provide a kind of aircraft taxi planing method, comprise step: the aircraft position data that receive the position of indication aircraft on the airport; First slide branch's menu according to what the airport slided that data generate and described aircraft position data match; The reception indication is slided first of branch from described first first selection of sliding branch's menu selection and is slided branch's selection signal; Slide data and described first according to described airport and select to slide that branch generates and described first selection slides that branch matches second slides branch's menu; The reception indication is slided second of branch from described second second selection of sliding branch's menu selection and is slided branch's selection signal; Generate indication described second and select to slide the taxi circuit of branch; And a sliding path signal of the described sliding path of indication is sent to display system.
Very clear, the present invention obviously improves prior art systems.In addition, the insider can be appreciated that the restriction that is not subjected to use FMS.In realizing the present invention, can use other processor, display screen and data input part part.
Other characteristics of the present invention and advantage are set forth in the detailed description of back, illustrate that from this a part of characteristics and advantage are significantly for the insider, and can recognize other characteristics and advantage by implementing the present invention according to detailed description, claims and each the description of the drawings of back.
Should to understand above-mentioned explanation be exemplary for the present invention and be used for providing general introduction to character of the present invention and the feature understood by claims definition.Also comprise accompanying drawing so that further understand the present invention, these accompanying drawings constitute the part of explanation.These accompanying drawings illustrate various feature of the present invention and embodiment, and they and description of them are explained principle of the present invention and operation together.
Description of drawings
Fig. 1 is the calcspar according to an embodiment of taxi planning system of the present invention;
Fig. 2 is according to the index pages of setting out/arrive that shows on MCDU of the present invention;
Fig. 3 slides the planning page according to of the present invention setting out;
Fig. 4 is an example that slides the planning page according to arrival of the present invention;
Fig. 5 is an example that slides the planning page according to arrival of the present invention;
Fig. 6 A and 6B illustrate the table that the chained list by foundation one embodiment of the invention constitutes;
Fig. 7 illustrates the chained list according to one embodiment of the invention; And
Fig. 8 is the process flow diagram of the algorithm of this chained list of search.
Embodiment
Now in detail with reference to each present preferred embodiment of the present invention, their example shown in the drawings.In case may, in these accompanying drawings, use identical reference number to indicate same or analogous part.
An example embodiment of foundation shown in Figure 1 taxi planning system of the present invention, it is briefly represented with reference number 10.
At first simply and then explain the ingredient of taxi planning system of the present invention.The most common application of the present invention is as aircraft, for example commercial passenger aircraft or jet cargo aircraft, FMS in an integration section, thereby following discussion will be with respect to this application note the present invention.
At first with reference to Fig. 1, shown in the figure according to the calcspar of an embodiment of taxi planning system of the present invention and relevant aircraft system.All aircraft systems can comprise the present invention, thereby they are collectively called taxi planning system 10.Taxi planning system 10 can comprise Flight Management Computer (FMC) 11, multi-functional control display unit (MCDU) 12, navigational route database (NDB) 13, leading display (HUD) 14, EFIS (EFIS) 15, multi-mode receiver (MMR) 16, transponder 17 and communications management unit (CMU) 18.FMC11 and MCDU12 are called flight management system (FMS) usually together.
FMC 11 comprises processor 11A and storer 11B.Processor 11A can comprise any data processor that is applicable to reception and processing command and data.Processor 11A preferably has the microprocessor of enough throughputs so that finish desired FMS in real time and slide planning tasks.Storer 11B preferably include be used for storing the random-access memory (ram) of dynamic data and variable and be used for program data and static data ROM (read-only memory) (ROM) the two.Processor 11A communicates by letter so that search program instruction and data and manipulation and storage of variables with storer 11B.Processor 11A also communicates by letter with NDB13.
NDB 13 comprises the airport of the airport installation of describing airfield runway, taxiway, landing gate, hardstand and various other needs and slides data.Data storage is slided in chained list 13A in these airports, and each bar standard taxi circuit 13B also is stored in this database.The airport is slided data and is comprised such data, for example, and the position of expression runway and the runway data of width, the taxiway data of the position of expression taxiway and the position of expression landing gate and the landing gate data of heading.NDB 13 is preferably rewritable or interchangeable, thereby thereby can be upgraded as required easily and these data comprise the change of at present relevant airfield runway, taxiway etc.NDB 13 makes up with any various memory storage techniques, for example the various combinations of PROM, EPROM, EEPROM, disc driver, CD drive or these and like.The chained list that illustrates later preferably is stored among the NDB 13.
Preferably realize user interface by the MCDU12 that communicates by letter with FMC 11 and processor 11A.MCDU12 comprises display screen 12A, row options button group 19 and keypad 12B.MCDU12 is generally used for to FMC 11 input airline operation programming commands and is used for by display screen 12A to driver, crew or operator's output route airplane data.The operation of each row options button 19 allows to select fast or deletion is shown item.The present invention preferentially utilizes this user interface component that has earlier to realize being used for the user interface of airport surface navigation, although also can utilize other user interface to realize the present invention.For example, if desired can for example EFIS 15 or HUD 14 be used as the part of this user interface other display.
HUD 14 is shown as by sliding path signal 11C with EFIS 15 and communicates by letter with FMC 11.Sliding path signal 11C comprises the data of expressing selected sliding path.HUD 14 is incident upon image on the combiner in the sight line the place ahead that is positioned at the driver, thus the driver can side by side watch this image and can from the preceding wind shelves of aircraft outwards see .EFIS 15 (being also referred to as HDD) typically be positioned at wind shelves before the aircraft below.EFIS 15 comprises one or more display screens, and they utilize the display unit of type on cathode ray tube (CRT), flat-panel monitor or the function to realize typically.When selecting to slide plan, be preferably on HUD 14 or the EFIS 15 and show this plan to the driver.
Several communication systems also are connected with FMC 11.MMR 16 receives navigation or position signalling, for example, and GPS (GPS) signal, differential GPS (DGPS), local strengthening system (LAAS) signal, wide area strengthening system (WAAS) signal or the like.These signals are sent to determines the FMC 11 of aircraft with respect to the position of each airport feature point thereon.Utilize then this aircraft-position information suitable for the driver calculates slide the selection option.
Transponder 17 and CMU 18 provide additional input/output communication passage.Transponder 17 for example can receive automatic dependent surveillance broadcasting (ADS-B) signal from other aircraft or ATC.CMU 18 have with ATC or and the link of the data of similar control management organization, plan of sliding and instruction communicate, consult, revise, ratify or refuse by it.
Fig. 2-5 illustrates user interface.User capture of the present invention is preferably finished by the DEP/ARR INDEX page as shown in Figure 2.Fig. 2 illustrates display screen 12A and row options button (LSK) group 19.Each row options button 19 identifies to 6L and 1R to 6R with 1L respectively, and they are used to select the option expected.To slide planning page driver and one of encourage among 2L, 2R or the 4R in order to visit.This demonstration expression one airplane is prepared to fly to the KATL airport from the KJFK airport.In order to be planned for the sliding path excitation LSK 2L that sets out of runway.To get back to landing gate in order planning, for example to force this aircraft to return KJFK, sliding path select LSK 2R.Raise the arrival sliding path from the taxiway to the landing gate of KMEM for the planning purpose diji and select LSK 4R.In case excitation LSK 2L, screen change into the KJFK shown in Fig. 3 and set out and slide the page.
The page is slided in setting out that utilization demonstrates, at first landing gate position and purpose runway up till now.This information can be called from storer again, receive, imported at current page in different FMS page inputs or by the driver by the driver from other aircraft system.If do not import this information as yet, by possible landing gate menu and then point out the position to the driver by possible runway menu.Select ground fully, the driver can be by the working area input landing gate of MCDU and the information of runway.After obtaining landing gate and runway, system visit NDB 13, calculate possible taxiway and/or linkage section menu and on the screen 12A of contiguous LSK 19, show them.From the selection of this possible taxiway and/or linkage section menu, the next new menu that may select appears under " TO " title along with at every turn.The selected clauses and subclauses of blast and " TO " title fall and prepare the space with the top at " TO " title for these selected clauses and subclauses.This page scroll-up/down is to show suitable information.Select the clauses and subclauses of blast to rebulid menu and eliminate this selector bar previous clauses and subclauses now once more once more for these clauses and subclauses.Continue this processing up to obtaining the purpose runway.After obtaining the two data of landing gate and runway, " STD ROUTE " near LSK 5R, occur and select.Canonical path is selected automatically to select predefined sliding path menu, thereby can select from current position to the destination sliding path under one-keystroke.Preferably reach definite suitable menu selection by chained list and the algorithm that uses the back.
Fig. 4 illustrates the arrival page according to one embodiment of the invention.Can be by setting out/arriving on the index pages, for example shown in Fig. 2, excitation LSK 4R enters the arrival page.As top discussion, determine runway and landing gate information.Processor 11A visits NDB 13 and calculates possible taxiway and the menu of linkage section, selects along with carry out menu at every turn, calculates the new menu that may slide selection and demonstration below " TO " title.Selected clauses and subclauses blast and " TO " title fall so that be this selected clauses and subclauses preparation space.Select the clauses and subclauses of blast to rebulid menu and eliminate this selector bar previous clauses and subclauses now once more once more for these clauses and subclauses." STD ROUTE " prompting appears after obtaining runway and landing gate information.
Fig. 5 illustrates an example menu of possible taxiway and linkage section.
As shown, this possible taxiway is selected to be made of each crossing L5, L6, M4 and M5.Letter and number to distribution such as each bar runway, taxiway, linkage sections is unique to each airport and is stored among the chained list 13A of NDB 13.
Another aspect of the present invention is to realize the employed database of taxi planning system of the present invention.This database slides data for each storage airport, airport.In order to realize that this aspect of the present invention preferably adopts chained list.At chained list shown in Fig. 6 A, 6B and 7.Two data watch chains are connected together.First table is sliding path ID table (TPIDT) 71, and this table comprises sliding path ID record (TPIDR) 61.
TPIDR 61 comprises identifier field 61A, for example be used for a runway 36L, be used for the A16 of a landing gate or be used for the L5 of a taxiway linkage section.Slide type field 61B sign current path for example runway, taxiway, hardstand, landing gate or similar traffic pattern.Pointer field 61C is to sliding some the link of record (TPR) 62 of sliding among table (TPT) 72, and TPT table 72 comprises related respectively the sliding a little with this sliding path ID.Number field 61D tell program this slide a little the numbering of sliding of ID.
Second TPT 72 that table is made up of TPR 62.Each TPR 62 comprises the latitude field 62A and the longitude field 62B of the horizontal level that is used for accurately stipulating this point.Width field 62C stipulates the road face width degree of this point.Height field 62D comprises the height of this point.It can be an absolute altitude or with respect to the relative position of reference point in the airport or markstone.Vertex type field 62E presses special characteristic (for example, the part on curved surface or the flat face, holding point or landing gate) and identifies this point.Some point causes specific action.For example HOLD (maintenance) point keeps system alert driver approval before continuing.This preferably by stop display screen advance or the display screen that rolls keeps realizing by encouraging 19 approvals of a capable options button until the driver.
Slide a record and comprise the link 62F that points to the pointer of the record among the TPIPT 71 on another mark.For example, if an airplane is arranged, typically there are many linkage sections on runway to each taxiway.Utilize this pointer field, taxiway that processor 11A is can quick identification possible and linkage section and set up that a confession shows on menu suitably slide branch's menu.
Chained list between these two tables shown in Figure 7.Each record among the TPIDT 71 comprises the link of a record to the TPT 72.They are indicated with link 71A and 71B.Similarly, the many records among the TPT 72 contain the link of a plurality of records to TPIDT 71.This illustrates by link 72A and 72B, they illustrate from record TPR 1 to two links of writing down TPIDR 4 and TPIDR N-3.
Adopt list structure to allow suitable the sliding of quick identification of the present invention to select and allow the driver to set up by the plan of forming of sliding of sliding among the NDB 13 fast.
Utilize flow process 80 that method of the present invention is shown among Fig. 8, after starting frame 81 beginnings, this method enters frame 82 and receives the current location of aircraft on the airport.Preferably import data and finish this step by the driver.The driver also can import these data in the way of airport of destination of flying to.This step can also comprise and receives destination locations in a similar manner.On the contrary, can by with the automaticdata of ATC link receive these data or according to come self aligning system for example the position data of GPS determine this data.
This method enters frame 83, wherein from the related sliding path ID record of NDB retrieval.For example, if aircraft on runway 27R, is then retrieved the sliding path ID record that is used for 27R.This sliding path ID record comprises one to the related pointer that slides a record, and these slide a record and comprise for example each location point of runway and the data of width.
In frame 84, retrieve a related record that slides.These slide a record and comprise possible sliding a little for suitably sliding the taxiway of branch and the pointer of linkage section specific.This method enters frame 85, wherein utilizes each pointer that points to different sliding path records to determine possible taxiway and linkage section.May there be a plurality of pointers to different sliding path ID records.This method continues at frame 86, and wherein each bar taxiway and linkage section form a selection menu and show on display screen.At frame 87, receive the user and stipulate the taxiway expected or the input of linkage section.
This method continues at decision box 88, checks wherein whether selected taxiway or linkage section are to stop branch.For example, if this selection is a landing gate, then imagination is finished the taxi circuit plan and is finished this processing.If not this situation, this processing turns back to frame 84 and continues, and wherein retrieves a suitable relevant record that slides once more.Continue this processing, before the conventional terminating point of arrival, stop this plan until finishing plan of sliding or driver.When selecting this sliding path, on HDD, show this path and be superimposed upon above the airport map at frame 89, thus the understanding that the driver is improved to situation.
The insider is clear, under the spirit or scope of the present invention that does not deviate from by the definition of appended claims book, can make various modifications to the illustrated the preferred embodiments of the present invention of this paper.
Claims (20)
1. aircraft taxi planning system comprises:
A user interface comprises:
A display screen, and
Select input for one;
The data storage part of data is slided on a storage airport; And
The processor of one and described display screen and described selection input communication,
Wherein said processor slides the previous branch of sliding of data and according to described airport and selects to generate and may slide branch's menu, and described processor is sent to described display screen with described menu, describedly slides branch and the aircraft position matches.
2. aircraft taxi planning system as claimed in claim 1, wherein said airport slide data and comprise runway data, taxiway data and landing gate data.
3. aircraft taxi planning system as claimed in claim 1, wherein said data storage part are stored predefined standard taxi circuit.
4. aircraft taxi planning system as claimed in claim 1, data are slided by storage of linked list in wherein said airport.
5. aircraft taxi planning system as claimed in claim 1 is led display system under wherein said display screen comprises.
6. aircraft taxi planning system as claimed in claim 1, wherein said display screen comprises leading display system.
7. aircraft taxi planning system as claimed in claim 1, wherein said display screen are to select from the group of being made up of EFIS, leading display, transponder and wireless communication system.
8. aircraft taxi planning system as claimed in claim 1, wherein said user interface comprise a multi-functional control display unit.
9. aircraft taxi planning system as claimed in claim 1, wherein said processor comprises Flight Management Computer.
10. aircraft taxi planing method comprises step:
Receive the aircraft position data of the position of indication aircraft on the airport;
First slide branch's menu according to what the airport slided that data generate and described aircraft position data match;
The reception indication is slided first of branch from described first first selection of sliding branch's menu selection and is slided branch's selection signal;
Slide data and described first according to described airport and select to slide that branch generates and described first selection slides that branch matches second slides branch's menu;
The reception indication is slided second of branch from described second second selection of sliding branch's menu selection and is slided branch's selection signal;
Generate indication described second and select to slide the taxi circuit of branch; And
The sliding path signal of the described sliding path of indication is sent to display system.
11., also comprise the step of the aircraft destination data that receives the destination locations on the described airport of indication as the aircraft taxi planing method of claim 10.
12. as the aircraft taxi planing method of claim 10, wherein this first generation step comprises generation standard taxi circuit.
13. as the aircraft taxi planing method of claim 10, wherein each step that generates menu comprises that searching for the airport slides the chained list of data.
14. as the aircraft taxi planing method of claim 13, wherein said chained list comprises and slides a table.
15. as the aircraft taxi planing method of claim 13, wherein said chained list comprises sliding path ID table.
16. the aircraft taxi planing method as claim 10 also comprises the step that described sliding path is sent to ground control system.
17. as the aircraft taxi planing method of claim 13, wherein said chained list comprises the vertex type field.
18. as the aircraft taxi planing method of claim 17, wherein said vertex type field comprises HOLD (maintenance) value.
19. as the aircraft taxi planing method of claim 18, also comprise according to described aircraft near with related the sliding a little of described HOLD value, ask the step of an action by the driver.
20. as the aircraft taxi planing method of claim 10, wherein said display system is from selecting by leading down the group that display system and leading display system form.
Applications Claiming Priority (11)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US33719201P | 2001-12-04 | 2001-12-04 | |
| US33729501P | 2001-12-04 | 2001-12-04 | |
| US33718201P | 2001-12-04 | 2001-12-04 | |
| US33675201P | 2001-12-04 | 2001-12-04 | |
| US60/337,182 | 2001-12-04 | ||
| US60/337,192 | 2001-12-04 | ||
| US60/336,752 | 2001-12-04 | ||
| US60/337,295 | 2001-12-04 | ||
| US10/078,703 US6751545B2 (en) | 2001-12-04 | 2002-02-20 | Aircraft taxi planning system and method |
| US10/078,703 | 2002-02-20 | ||
| PCT/US2002/034735 WO2003048886A2 (en) | 2001-12-04 | 2002-10-30 | Aircraft taxi planning system and method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1742277A CN1742277A (en) | 2006-03-01 |
| CN1742277B true CN1742277B (en) | 2010-05-12 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN02824336.6A Expired - Lifetime CN1742277B (en) | 2001-12-04 | 2002-10-30 | Aircraft taxi planning system and method |
| CNB028243560A Expired - Fee Related CN100555358C (en) | 2001-12-04 | 2002-10-30 | Airport map display system and method for interchanging data |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB028243560A Expired - Fee Related CN100555358C (en) | 2001-12-04 | 2002-10-30 | Airport map display system and method for interchanging data |
Country Status (1)
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|---|---|
| CN (2) | CN1742277B (en) |
Families Citing this family (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8090483B2 (en) * | 2010-02-15 | 2012-01-03 | Honeywell International Inc. | System and method for displaying control related information to an aircraft operator |
| CN102004852B (en) * | 2010-11-18 | 2012-06-27 | 南京莱斯信息技术股份有限公司 | Airport ground aircraft slide route automatic calculating method |
| US9013330B2 (en) * | 2011-09-01 | 2015-04-21 | Honeywell International Inc. | Electric taxi system guidance |
| US8676399B2 (en) * | 2011-11-21 | 2014-03-18 | Honeywell International Inc. | System and method for generating and displaying an electric taxi index |
| CN102522064B (en) * | 2011-12-14 | 2014-01-29 | 中国航空无线电电子研究所 | Cabin controller with color OLED (Organic Light Emitting Diode) display screen |
| US20130321169A1 (en) * | 2012-05-30 | 2013-12-05 | Honeywell International Inc. | Airport surface collision-avoidance system (ascas) |
| US9092976B2 (en) * | 2012-09-14 | 2015-07-28 | Honeywell International Inc. | Systems and methods for providing runway-entry awareness and alerting |
| US9074891B2 (en) * | 2012-10-18 | 2015-07-07 | Honeywell International Inc. | High integrity, surface guidance system for aircraft electric taxi |
| US9058742B2 (en) * | 2013-02-12 | 2015-06-16 | Ge Aviation Systems, Llc | Methods for illustrating aircraft situational information |
| US9082301B2 (en) * | 2013-10-28 | 2015-07-14 | The Boeing Company | Aircraft stopping performance display and warning |
| US9666085B2 (en) * | 2014-11-14 | 2017-05-30 | Honeywell International Inc. | Methods and systems for displaying a taxi clearance |
| US9786186B2 (en) * | 2014-11-18 | 2017-10-10 | Honeywell International Inc. | System and method for confirming received taxi instructions |
| FR3051057B1 (en) * | 2016-05-04 | 2021-11-26 | Thales Sa | PROCESS FOR AUTOMATICALLY JOINING A VERTICAL REFERENCE PROFILE OF AN AIRCRAFT |
| EP3407330A1 (en) * | 2017-05-23 | 2018-11-28 | ADB Safegate Sweden AB | Control system at an airport |
| CN110322775B (en) * | 2019-05-30 | 2021-06-29 | 广东省机场管理集团有限公司工程建设指挥部 | Airport information display method and device, computer equipment and storage medium |
| CN115294807B (en) * | 2022-09-28 | 2022-12-27 | 四川腾盾科技有限公司 | Control method for intelligent selection of exit of contact crossing for large unmanned aerial vehicle |
-
2002
- 2002-10-30 CN CN02824336.6A patent/CN1742277B/en not_active Expired - Lifetime
- 2002-10-30 CN CNB028243560A patent/CN100555358C/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CN100555358C (en) | 2009-10-28 |
| CN1771524A (en) | 2006-05-10 |
| CN1742277A (en) | 2006-03-01 |
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